NORSAT 4, 62702
Orbit data source: Space-Track
NORSAT 4, 62702 is a payload satellite owned by NSC (NO) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62702 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
UTIAS-SFL
Mission
Operational Civil Com/Tech
Bus & Motor
DEFIANT, Unknown motor
Mass
35 kg wet, 35 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.6 m
Radar Cross Section
0.165 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 NORSAT 4
1 62702U 25009CX 25293.21148545 .00005055 00000-0 48328-3 0 9997
2 62702 97.7275 11.0521 0002886 109.2975 250.8557 14.93678019 41525Epoch: 2025-10-20T05:04Z
TLE epoch observation values (Epoch: 2025-10-20T05:04:32.342Z)
Latitude
-0.00007°
Longitude
-93.9997°
Altitude
590.184 km
Speed
7.565 km/s
True Right ascension
00h 44m 12s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
10:56:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.503 km
Perigee altitude
581.485 km
Semi-major axis
6,961.631 km
Eccentricity
0.00029
Inclination
97.7275°
RAAN
11.0521°
Arg. of periapsis
109.2975°
True anomaly
250.82446°
Mean anomaly
250.8557°
Eccentric anomaly
250.84008°
Mean motion
3.7366 °/min
Orbital period
96.34 mins
BSTAR
0.00048328
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.NORSAT 4 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-20 18:31:16.714Z | 352.41° N | 2025-10-20 18:33:16.714Z | 293.698° NW | 38.793° | 2025-10-20 18:37:16.714Z | 209.456° SW |
| 7 mins | 2025-10-21 05:19:16.714Z | 165.852° S | 2025-10-21 05:22:16.714Z | 122.774° SE | 44.979° | 2025-10-21 05:26:16.714Z | 348.112° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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